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THE MoTIS AIR BENDER


THE MoTIS VERT-LEV PROJECT

EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT

INTRODUCTION:

A COMPLETE CASE STUDY INTO THE THEORY OF FIXED PITCH WHIRLING WING PROPS AND THERE POTENTIAL USE IN INTERSTATE MASS AERIAL TRANSPORT

BY

TEAM MoTIS DEVELOPMENT STAFF

 

 

ELECTRONIC TABLE OF CONTENTS


  • AIRCRAFT INTRO

  •  

  • THE ACTUAL AIR RAIL SYSTEM

  •  

  • THE ACTUAL NEO CONCEPT AIRCRAFT TECHNOLOGY

  •  

  • GRAPHICS REPRESENTATIONS OF AIRCRAFT

  •  

  • HOW THE AIR BENDER TRANSPORTER WORKS

  •  

  • VERT-LEV THEORY MATH

  •  

  • PROJECT GALLERY

  •  

  • EXCEL DATA DEPARTMENT

 


INTRODUCTION:

A COMPLETE CASE STUDY INTO THE THEORY OF FIXED PITCH WHIRLING WING PROPS AND THERE POTENTIAL USE IN INTERSTATE MASS AERIAL TRANSPORT

BY

TEAM MoTIS DEVELOPMENT STAFF

 

 

 

 

 

 

 

 


   AIRCRAFT INTRO:

Welcome to the first day of posted information on what will become known to you as the VERTICAL MASS TRANSITS INTERSTATE LEVITATION SYSTEM.

The VERT-LEV system is a complete virtual study developed by team MoTIS internal staff on a super cheap and fuel efficient aerial mass transit system! We have been working on this system, using flight simulations to test out our virtual theoretical logistics systems and are now ready to share with our viewing and buying public!

This whole logistical system comes almost entirely out of the mind of  MoTIS CEO and founder. O WATSON is the official developer of the AIR BENDER aircraft at AIR RAIL LOGISTICS SYSTEM, along with Jennifer Guess.  This is in no way a recreation of any kind and is a total and original concept logistical system being simulated into the world of Microsoft Flight Simulator platform programs.

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EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT

THE ACTUAL AIR RAIL SYSTEM

So what is this VERT-LEV project all about, you may ask? Well the goal of VERT -LEV is to research, design, and develop a cost effective solution to a potential and realistic mass interstate transportations system. team MoTIS has coined this concept the MoTIS MASS TRAN AIR RAIL SYSTEM.- MO-MATARS for short.

 The MoTIS development staff has already started building the virtual scenery infrastructure to support this intensive research study. The ideology is that we have already got numerous GPS satellites in orbit around the planet, and we are going to use this technology Virtually that is) to design a safe interstate ultra low altitude high way in the sky. This will become the actual AIR RAIL system itself.

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THE ACTUAL NEO CONCEPT AIRCRAFT TECHNOLOGY

Team MoTIS has long had a VTOL development wing operation at our virtual XROW labs, and have just recently decided on an interesting piece of VTOL/STOL equipment to do the job with in this type of mass transportation system.

Welcome the MoTIS AIR BENDER SUPER STOL UTILITY VEHICLE.

NOTES: COMING


Graphical Representations:

FULL DATA COMING SOON

 

 

 

 

 

 

 

 


As there are numerous was to convey information in then present age of information, we at team MoTIS are adopting a new and efficient way o f sharing our data and info with you. Only known as the E-BOOK CONCEPT, we will be totally abandoning any presentations in standard PDF format, and word document format , for what most online surfers are already use to! The HTML online style layout.  THE E-BOOK CONCEPT is not a new concept in the since that it is something new, but in the since that we are creating a certain style and presents to our information layouts that will be presented to you in this complete actual online book layout format. We will present you with numerous book cover jackets, graphic binders, and more! Best of all the note book in the FS program that we develop for will allow you to open any and all of our materials right inside your cockpit so that you can read on those long flight! 

AIRCRAFT SPECS:

THE VERT-LEV PORT CONCEPT


Graphical Representations:

 

 

FS FLIGHT DATA NOTES

This aircraft has not been tested in X PLANE or flight simulator 2004 due to challenges in simulating an accurate flight dynamics CFG file model for this aircraft in question. We are working to create this dynamics model by creating addition variable on the CFG file that will accurately simulate our mathematical flight parameters.  We need to simulate an independent vertical mounted fixed pitch wing prop with reasonable drag dimensions and high lift out puts on throttle up. That can be sustained against the induced drag of forward flight without significant loss in to vertical lift out puts to support the weight of the aircraft. While avoiding simulated yaw moments as the whirling wing is balanced with a coaxial counter rotating whirling wing.  Also to have independent thrusting from the main forward prolusion engine mounted in the rear of the VERT-LEV.

 


EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT

SWIRLUX AIR TORQUE 2000

This AIR BENDER is s super unique research aircraft in the fact that is not a helicopter, and not a true VTOL aircraft, but is instead a partial whirling fixed wing lift device conceived by team MoTIS development staff. Here is a break down of where the VERT-LEVS would fall under a general current standard aircraft category of today.

CHOPPER GYRO PLANE HELIPLANE VERT-LEVS STOL AIRCRAFT TRUE VTOL

This aircraft is solely designed to operate with in the AIR RAIL SYSTEM and is not classed as a general purpose aircraft at all. The VERT -LEVS are to be classified as SUPER STOL aircraft. These aircraft can best be described as rotating wings! As the aircraft have now VTOL dynamics at all. Their over all usefulness is in the fact that they can take off and land in almost nonsensically short distances! This SUPER STOL dynamics performance characteristic will allow for special VEER-LEV aircrafts to be built on top of existing buildings as totally new VERT LEV airports.

The VERT -LEV theoretical principle is simple. Use a Hugh high density whirling wing to generated the needed take off lift , and use a standard pusher thrust producing device to propel the aircraft into forward flight! The aircraft generate what is virtual suspected as a lift cylinder, which is totally controlled via a special throttle and governor built into the engine. The aircraft generates excessive vertical lift and then with the help of special stabilizers placed around the aircraft, is lifted genially into the heavens!. There are two sets of throttles in the VERT-LEVS. One controls the lifting turbine engine and the other the horizontal thrusting turbine.

This type of aircraft is governed totally by the amount of lift that can be generated by engine out put values.


AIRCRAFT STABILITY CONTROLS

The aircrafts lack wings and are all controlled by multiple stabilizer projects out of the sides of the fuselage.

ROLL MOMENTS

PITCH MOMENTS

 

 

 

 

 

 

 

 


HOW THE AIR BENDER TRANSPORTER WORKS

First of all the VERT-LEVS do not exhibit any VTOL abilities what so ever. These aircraft lack full physical fixed wings and instead generate all lift for two counteracting high density high pitched whirling wing units!

THE AERODYNAMICS EQUILIBRIUM BALANCING ACT

This principle works exactly like a standard propeller accept the fact that the SWIRLUX unit is massive and needs to generate very small RPMS to generate excessive lift capacities, due to the radius of the WING PROP lifting blades. the aircraft fly's exactly like a conventional fixed wing aircraft except the fact that she is SUPER STOL capable!

The AIR BENDER first achieves the right among of RPM, which give you the proper amount of actual lift generated above the aircraft, the aircraft is fully flight ready!

MASSIVE PROOF OF CONCEPT COMING SOON VIA EXCEL DATA LABS

 

THE MoTIS VERT-LEV PROJECT

SAMPLE 2D FLUID ANALYSIS PRODUCED BY ARIEL G

AIR BENDER TAKE OFF PERFORMANCE SPECS

The AIR BENDER will have the ability to carry mass passenger and cargo loads and to transition from ground operations and into flight very quickly. The standard rating cycle for the lift generation system needs to generate at approximately  25% above maximum allowable loaded take off weights. The aircraft is therefore designed with greater engine out put then the over all weight of the aircraft, providing power stroke torque inputs into the fixed Wing/Prop blades

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EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT

 PANEL AND VISIBILITY

Sample first stage panel documentation

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VERT-LEV THEORY MATH

In theory let us say that the aircraft weights 3500lbs and the turbine is generation a turbine shaft torque of 3000 RPMS. each RPM setting has a total lift setting. So at maximum RPM the total lifting capacity of the VERT-LEVS give us a new lift rating in this particular neo concept aircraft in question, known as VLT max.

For all of our theoretical study models using X PLANE and MSFS we will rate this total lifting capacity at 25% of the total weight of our aircraft in question.

If our VERT-LEV lets say weights 3500 lbs then our VLT max lift rating will be 3500 x .25= 875 lbs lift excess on this particular aircraft.3500 + 875= 4375lbs this concept actually gives each aircraft super torque lifting capacities.

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GUTS TECHNICAL DRAWING :

The first guts system to preview on this aircraft will be the AIR BENDER custom gear system, now under development by GUTS primary designer.

AIRCRAFT SUB-SYSTEMS

Our resident CATIA developer is working on a great new great system design for the MoTIS AIR BENDER neo concept aircraft! This gear system will be fully developed in AUTO CAD, CATIA, and FSDS V3!

 

 

 

 

E BOOK END COVER

CREDITS AND EXTENDED SUBJECT

 

 

 

 

 

 

 

 

 

 

ADDITIONAL ATTENTION: Please member that team MoTIS is fueled with college students and real world aerodynamics students and our mission is not simulated for the pure hobbyist only.

NOTICE: This experimental aircraft is not a helicopter, gyroplane, convertiplane, or heliplane. It is a virtual study in a theoretical whirling winged aircraft. The CO-AXIAL MOUNTED WING-PROP- AKA TWISTERS, as we are defining it, is a lift generating device that the team MoTIS development staff if working on mathematical proximity equations for. We will post this data in full at the end of the study in the form of an online case study paper in word perfect. This is an original idea and the intellectual property of team MoTIS development staff. All rights reserved.

Note: All of these concept aircraft and experimental logistics systems are from the design staff of the MoTIS CAD engineering board and our CEO. We do not copy others work or design real world concept aircraft at all. Each of our aircraft are from our heads and are the sole intellectual property of MoTIS and we can prove it. We take great pride in all of our true concept designs and do not create real world aircraft, model aircraft variants or concepts, or other designers concept work at all ,but stand by our mission statement in truly creating "OUR OWN DESIGNS"

MoTIS VIRTUAL  JET DESIGN is a leading virtual FS neo concept aircraft manufacturer with the most modern and extensive product line.